Cover image for Space electronic reconnaissance : localization theories and methods
Title:
Space electronic reconnaissance : localization theories and methods
Uniform Title:
Kong jian dian zi zhen cha ding wei yuan li. English
Publication Information:
Singapore, : John Wiley & Sons Singapore Pte. Ltd., 2014
Physical Description:
xix, 357 pages : illustrations ; 25 cm
ISBN:
9781118542194

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30000010338238 UG1520 S63 2014 Open Access Book Book
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Summary

Summary

Presents the theories and applications of determining the position of an object in space through the use of satellites

As the importance of space reconnaissance technology intensifies, more and more countries are investing money in building their own space reconnaissance satellites. Due to the secrecy and sensitivity of the operations, it is hard to find published papers and journals on the topic outside of military and governmental agencies. This book aims to fill the gap by presenting the various applications and basic principles of a very modern technology. The space electronic reconnaissance system in mono/multi-satellite platforms is a critical feature which can be used for detection, localization, tracking or identification of the various kinds of signal sources from radar, communication or navigation systems.

Localization technology in space electronic reconnaissance uses single or multiple satellite receivers which receive signals from radar, communication and navigation emitters in the ground, ocean and space to specify the location of emitter. The methods, principles and technologies of different space electronic reconnaissance localization systems are introduced in this book, as are their performances, and the various methods are explained and analysed. Digital simulations illustrate the results.

Presents the theories and applications of determining the position of an object in space through the use of satellites Introduces methods, principles and technologies of localization and tracking in the space electronic reconnaissance system, the localization algorithm and error in satellite system and near space platform system, and the tracking algorithm and error in single satellite-to-satellite tracking system Provides the fundamentals, the mathematics, the limitations, the measurements, and systems, of localization with emphasis on defence industry applications

Highly relevant for Engineers working in avionics, radar, communication, navigation and electronic warfare.

Chapters include:- the introduction of space electronic reconnaissance localization technology, knowledge about the satellite orbit and basic terminology of passive localization, single satellite geolocation technology based on direction finding, three-satellite geolocation technology based on time difference of arrival (TDOA), two-satellite geolocation technology based on TDOA and frequency difference of arrival (FDOA), the single satellite localization technology based on kinematics theory, localization principles of near-space platform electronic reconnaissance systems, the orbit determination of single satellite-to-satellite tracking using bearings only(BO) information, the orbit determination of single satellite-to-satellite tracking using bearings and frequency information, the orbit determination of single satellite-to-satellite tracking using frequency only(FO) information. Each chapter ends with a problem and solution section, some using Matlab code.


Author Notes

Fucheng Guo, National University of Defense Technology, P.R. China
Yun Fan, National University of Defense Technology, P.R. China
Yiyu Zhou, National University of Defense Technology, P.R. China
Caigen Zhou, National University of Defense Technology, P.R. China
Qiang Li, National University of Defense Technology, P.R. China


Table of Contents

Prefacep. xiii
Acknowledgmentsp. xv
Acronymsp. xvii
1 Introduction to Space Electronic Reconnaissance Geolocationp. 1
1.1 Introductionp. 1
1.2 An Overview of Space Electronic Reconnaissance Geolocation Technologyp. 3
1.2.1 Geolocation of an Emitter on the Earthp. 3
1.2.2 Tracking of an Emitter on a Satellitep. 8
1.2.3 Geolocation by Near-Space Platformsp. 9
1.3 Structure of a Typical SER Systemp. 9
Referencesp. 11
2 Fundamentals of Satellite Orbit and Geolocationp. 13
2.1 An Introduction to the Satellite and Its Orbitp. 13
2.1.1 Kepler's Three Lawsp. 13
2.1.2 Classification of Satellite Orbitsp. 15
2.2 Orbit Parameters and State of Satellitep. 18
2.2.1 Orbit Elements of a Satellitep. 18
2.2.2 Definition of Several Arguments of Perigee and Their Correlationsp. 20
2.3 Definition of Coordinate Systems and Their Transformationsp. 21
2.3.1 Definition of Coordinate Systemsp. 21
2.3.2 Transformation between Coordinate Systemsp. 25
2.4 Spherical Model of the Earth for Geolocationp. 27
2.4.1 Regular Spherical Model for Geolocationp. 21
2.4.2 Ellipsoid Model of the Earthp. 27
2.5 Coverage Area of a Satellitep. 30
2.5.1 Approximate Calculation Method for the Coverage Areap. 30
2.5.2 Examples of Calculation of the Coverage Areap. 31
2.5.3 Side Reconnaissance Coverage Areap. 33
2.6 Fundamentals of Geolocationp. 33
2.6.1 Spatial Geolocation Planep. 34
2.6.2 Spatial Line of Position (LOP)p. 34
2.7 Measurement Index of Geolocation Eitorsp. 38
2.7.1 General Definition of Errorp. 38
2.7.2 Geometrical Dilution of Precision (GDOP)p. 40
2.7.3 Graphical Representation of the Geolocation Errorp. 40
2.7.4 Spherical Error Probability (SEP) and Circular Error Probability (CEP)p. 41
2.8 Observability Analysis of Geolocationp. 44
Referencesp. 45
3 Single-Satellite Geolocation System Based on Direction Findingp. 47
3.1 Direction Finding Techniquesp. 47
3.1.1 Amplitude Comparison DP Techniquep. 48
3.1.2 Interferometer DF Techniquep. 40
3.1.3 Array-Based DF Techniquep. 55
3.1.4 Other DF Techniquesp. 57
3.2 Single-Satellite LOS Geolocation Method and Analysisp. 57
3.2.1 Model of LOS Geolocationp. 57
3.2.2 Solution of LOS Geolocationp. 59
3.2.3 CRLB of the LOS Geolocation Errorp. 60
3.2.4 Simulation and Analysis of the LOS Geolocation Errorp. 62
3.2.5 Geometric Distribution of the LOS Geolocation Errorp. 63
3.3 Mullitimes Statistic LOS Geolocationp. 64
3.3.1 Single-Satellite Mullitimes Triangulationp. 65
3.3.2 Average for Single-Satellite Multitimes Geolocationp. 66
3.3.3 Weighted Average for Single-Satellite Multitimes Geolocationp. 67
3.3.4 Simulation of Single Satellite LOS Geolocationp. 67
3.4 Single HLO Satellite LOS Geolocationp. 73
3.4.1 Analysis of Single GEO Satellite I OS Geolocationp. 73
3.4.2 Geosynchronous Satellite Multitimes LOS Geolocationp. 74
Referencesp. 77
4 Multiple Satellites Geolocation Based on TDOA Measurementp. 79
4.1 Three-Satellite Geolocation Based on a Regular Spherep. 80
4.1.1 Three-Satellite Geolocation Solution Methodp. 80
4.1.2 Multisatellite TDOA Geolocation Methodp. 82
4.1.3 CRLB of a Multisatellite TDOA Geolocation Errorp. 85
4.1.4 Osculation Error of the Spherical Earth Modelp. 86
4.2 Three-Satellite Geolocation Based on the WGS-84 Earth Surface Modelp. 88
4.2.1 Analytical Methodp. 89
4.2.2 Spherical Iteration Methodp. 92
4.2.3 Newton Iteration Methodp. 94
4.2.4 Performance Comparison among the Three Solution Methodsp. 96
4.2.5 Altitude Input Location Algorithmp. 100
4.3 Ambiguity and No-Solution Problems of Geolocationp. 102
4.3.1 Ambiguity Problem of Geolocationp. 102
4.3.2 No-Solution Problem of Geolocationp. 106
4.4 Error Analysis of Three-Satellite Geolocationp. 109
4.4.1 Analysis of the Random Geolocation Errorp. 109
4.4.2 Analysis of Bias Caused by Altitude Assumptionp. 112
4.4.3 Influence of Change of the Constellation Geometric Configuration on GDOPp. 114
4.5 Calibration Method of the Three-Satellite TDOA Geolocation Systemp. 117
4.5.1 Four-Station Calibration Method and Analysisp. 117
4.5.2 Three-Station Calibration Methodp. 125
Referencesp. 130
5 Dual-Satellite Geolocation Based on TDOA and FDOAp. 133
5.1 Introduction of TDOA-FDOA Geolocation by a Dual Satellitep. 133
5.1.1 Explanation of Dual Satellite Geolocation Theoryp. 133
5.1.2 Structure of Dual-Satellite TDOA FDOA Geolocation Systemp. 134
5.2 Dual LEO Satellite TDOA-FDOA Geolocation Methodp. 136
5.2.1 Geolocation Modelp. 136
5.2.2 Solution Method of Algebraic Analysisp. 138
5.2.3 Approximate Anal vtical Method for Same-Orbit Satellitesp. 141
5.2.4 Method for Eliminating an Ambiguous Geolocation Pointp. 143
5.3 Error Analysis for TDOA-FDOA Geolocationp. 144
5.3.1 Analytic Method for the Geolocation Errorp. 144
5.3.2 GDOP of the Dual LEO Satellite Geolocation Errorp. 146
5.3.3 Analysis of Various Factors Influencing GDOPp. 151
5.4 Dual HKO Satellite TDOA-FDOA Geolocationp. 152
5.4.1 Dual Geosynchronous Orbit Satellites TDOA - FDOA Geolocationp. 152
5.4.2 Calibration Method Based on Reference Sourcesp. 155
5.4.3 C'alibration Method Using Multiple Reference Source?p. 159
5.4.4 Flow of Calibration and Geolocationp. 164
5.5 Method of Measuring TDOA and FDOAp. 165
5.5.1 The Cross-Ambiguity Functionp. 165
5.5.2 Tlieoretical Analysis on the TDOA TDOA Measurement Performancep. 166
5.5.3 Segment Correlation Accumulation Method for CAF Computationp. 168
5.5.4 Resolution of Multiple Signals of the Same Time and Same Frequencyp. 172
Referencesp. 174
6 Single-Satellite Geolocation System Based on the Kinematic Principlep. 177
6.1 Single-Satellite Geolocation Modelp. 177
6.2 Single-Satellite Single-Antenna Frequency-Only Based Geolocationp. 179
6.2.1 Frequency-Only Based Geolocation Methodp. 179
6.2.2 Analysis of the Geolocation Errorp. 180
6.2.3 Analysis of the Frequency-Only Based Geolocation Errorp. 181
6.3 Single-Satellite Geolocation by the Frequency Changing Rate Onlyp. 183
6.3.1 Model of Geolocation by the Frequency Changing Rate Onlyp. 183
6.3.2 CRLB of the Geolocation Errorp. 185
6.3.3 Geolocation Simulationp. 186
6.4 Single Satellite Single-Antenna TOA-Only Geolocationp. 186
6.4.1 Model and Method of TOA-Only Geolocationp. 186
6.4.2 Analysis of the Geolocation Errorp. 180
6.4.3 Geolocation Simulationp. 102
6.5 Single-Satellite Interferometer Phase Rate of Changing Only Geolocationp. 192
6.5.1 Geolocation Modelp. 192
6.5.2 Geolocation Algorithmp. 195
6.5.3 CRLB of the Geolocation Errorp. 196
6.5.4 Calculation Analysis of the Geolocation Errorp. 197
Referencesp. 201
7 Geolocation by Near-Space Platformsp. 203
7.1 An Overview of Geolocation by Near-Space Platformsp. 203
7.1.1 Near-Space Platform Overviewp. 203
7.1.2 Geolocation by the Near-Space Platformp. 204
7.2 Multi platform Triangulationp. 204
7.2.1 Theory of 2D Triangulationp. 204
7.2.2 Error Analysis for Dual-Station Triangulationp. 205
7.2.3 Optimal Geometric Configuration of Observersp. 207
7.3 Multiplatform TDOA Geolocationp. 211
7.3.1 Theory of Multi platform TDOA Geolocationp. 211
7.3.2 2D TDOA Geolocation Algorithmp. 212
7.3.3 TDOA Geolocation Using the Altitude Assumptionp. 215
7.3.4 3D TDOA Geolocation Algorithmp. 215
7.4 Localization Theory by a Single Platformp. 217
7.4 A Measurement Model of localizationp. 218
7.4.2 A 2D Approximate Localization Methodp. 219
7.4.3 MGEKF (Modified Gain Extended Kalman Filter) Localization Methodp. 221
7.4.4 Simulationp. 223
Referencesp. 225
8 Satellite-to-Satellite Passive Orbit Determination by Bearings Onlyp. 227
8.1 Introductionp. 227
8.2 Model and Method of Bearings-Only Passive Trackingp. 227
8.2.1 Mathematic Model in the Case of the Two-Body Problemp. 228
8.2.2 Tracking Method in the Case of the. Two-Body Modelp. 229
8.2.3 Mathematical Model Considering J 2 Perturbation of Earth Oblatenessp. 232
8.2.4 Tracking Method Considering J 2 Perturbation of Earth Oblatenessp. 233
8.3 System Observability Analysisp. 235
8.3.1 Description Method for System Observabilityp. 235
8.3.2 Influence of Factors on the State Equationp. 236
8.3.3 Influence of Factors on the Measurement Equationp. 237
8.4 Tracking Simulation and Analysisp. 239
8.4.1 Simulation in the Case of the Two Body Modelp. 241
8.4.2 Simulation Considering J2 Perturbation of Earth Oblatenessp. 251
8.5 Summaryp. 258
Referencesp. 259
9 Satellite-to-Satellite Passive Tracking Based on Angle and Frequency Informal ionp. 261
9.1 Introduction of Passive Trackingp. 261
9.2 Tracking Model and Methodp. 262
9.2.1 Mathematic Model in the Case of the Two-Body Modelp. 262
9.2.2 Tracking Method in the Case of the Two-Body Modelp. 263
9.2.3 Mathematical Models Considering J 2 Perturbation of Earth Oblatenessp. 266
9.2.4 Tracking Method Considering J 2 Perturbation of Earth Oblatenessp. 267
9.3 System Observability Analysisp. 268
9.3.1 Influence of Factors of the State Equationp. 269
9.3.2 Influence of Factors of the Measurement Equationp. 269
9.4 Simulation and Its Analysisp. 277
9.4.1 Simulation in the Case of the Two-Body Modelp. 278
9.4.2 Simulation Considering J 2 Perturbation of Earth Oblatenessp. 296
9.5 Summaryp. 308
Referencesp. 309
10 Satellite-to-Satellite Passive Orbit Determination Based on Frequency Onlyp. 311
10.1 The Theory and Mathematical Model of Passive Orbit Determination Bused on Frequency Onlyp. 313
10.1.1 The Theory of Orbit Determination Based on Frequency Onlyp. 313
10.1.2 The System Model in the Case of the Two-Body Modelp. 313
10.1.3 The System Model for J 2 Perturbation of Earth Oblatenessp. 315
10.2 Satellite-to-Satellite Passive Orbit Determination Based on PSO and Frequencyp. 317
10.2.1 Introduction of Panicle Swarm Optimization (PSO)p. 317
10.2.2 Orbit Determination Method Based on the PSO Algorithmp. 319
10.3 System Observability Analysisp. 320
10.3.1 Simulation Scenario 1p. 322
10.3.2 Simulation Scenario 2p. 323
10.3.3 Simulation Scenario 3p. 325
10.4 CRLB of the Orbit Parameter Estimation Errorp. 329
10.5 Orbit Detennination and Tracking Simulation and Its Analysisp. 333
10.5.1 Simulation in the. Case of the Two-Body Modelp. 334
10.5.2 Simulation in the Case of Considering the Perturbationp. 347
Referencesp. 348
11 A Prospect of Space Electronic Reconnaissance Technologyp. 349
Appendix Transformation of Orbit Elements, State and Coordinates of Satellites in Two-Body Motionp. 351
Indexp. 355